View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65150U 26145.35762610 +.00000000 +00000-0 +27312-3 0 00006
2 65150 51.9004 176.5650 0000670 326.6530 33.4390 14.80130077 09
| Epoch (UTC): | 25 May 2026 08:34:58 |
| Eccentricity: | 0.0000670 |
| inclination: | 51.9004° |
| perigee height: | 628 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 176.5650° |
| argument of perigee: | 326.6530° |
| revolutions per day: | 14.80130077 |
| mean anomaly at epoch: | 33.4390° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|